Installation Manual
Table Of Contents
- 17001_0_Frt-Matr
- 17001_1_Gen-Info
- 1.1 INTRODUCTION
- 1.2 FUNCTIONAL DESCRIPTION
- 1.2.1 Software Release Summary
- 1.2.2 Transponder Functional Overview
- 1.2.3 GPS Functional Overview
- 1.2.4 Lightning Detection (optional)
- 1.2.5 ADS-B System Overview
- 1.2.6 Traffic Display Functional Overview
- 1.2.7 FISB System Overview
- 1.2.8 Traffic Awareness System (option) Overview
- 1.2.9 ADS-B Traffic Advisory System Overview (optional)
- 1.2.10 Traffic Alert and Collision Avoidance System (option) Overview
- 1.2.11 Terrain Awareness and Warning System Overview (optional)
- 1.2.12 TerrainVisionTM
- 1.2.13 Discrete Inputs and Outputs Functional Overview
- 1.3 EQUIPMENT DESCRIPTIONS
- 1.4 INTERFACES
- 1.4.1 ADS-B Out Fail
- 1.4.2 AHRS Input
- 1.4.3 Altitude Encoder Input
- 1.4.4 Audio Out
- 1.4.5 Standby Mode
- 1.4.6 Audio Mute In and Out
- 1.4.7 Audio Acknowledge
- 1.4.8 RF Suppression Input/output
- 1.4.9 Traffic Alert
- 1.4.10 TAWS Caution and Warning Alert
- 1.4.11 WiFi Interface
- 1.4.12 WOW Input
- 1.4.13 Maintenance Interface
- 1.4.14 GPS Antenna
- 1.4.15 L-Band (978/1030/1090 MHz) Antenna
- 1.4.16 Directional Antenna
- 1.4.17 Traffic Display
- 1.4.18 Weather Display
- 1.4.19 Lightning Detection (WX-500)
- 1.4.20 Control Panel
- 1.5 INSTALLATION CONSIDERATIONS
- 1.6 SPECIFICATIONS
- 1.7 TSO INFORMATION
- 1.8 MODIFICATIONS
- 1.9 SOFTWARE REVISIONS
- 1.10 EQUIPMENT REQUIRED NOT SUPPLIED
- 1.11 EQUIPMENT INTERFACES
- 1.12 OBTAINING SOFTWARE
- 1.13 INSTALLATION PROCEDURE FOR LYNXMSS USB DRIVER
- 1.14 INSTALLATION APPROVAL AND LIMITATIONS
- 17001_2_Instal
- 2.1 INTRODUCTION
- 2.2 UNPACKING AND INSPECTING
- 2.3 INSTALLATION PROCEDURES
- 2.3.1 Panel Mount Location
- 2.3.2 Remote Mount Location
- 2.3.3 Electrical Connections
- 2.3.4 Compatible Equipment Installation Information
- 2.3.5 Discrete Inputs and Output Connections
- 2.3.6 Installation Guidelines for the DCM
- 2.3.7 P1 Mating Connector Assembly
- 2.3.8 Panel mount NGT-9000 Installation
- 2.3.9 Remote Mounted Lynx NGT-9000 Installation
- 2.3.10 CP-2500 Installation Guidelines
- 2.3.11 Antenna Installation Guidelines
- 17001_3_Inst_Check
- 3.1 INTRODUCTION
- 3.2 BASIC OPERATION
- 3.3 MPC (MAT) OPERATION
- 3.4 INSTALLATION PROCEDURE FOR LYNXMSS USB DRIVER
- 3.5 MAINTENANCE MODE
- 3.6 VERIFY SOFTWARE VERSION
- 3.7 SELECT CONFIGURATION OPTIONS
- 3.8 CALIBRATION SETUP
- 3.9 INTERFACE CHECK
- 3.10 SETUP PIM-9000 WIFI MODULE
- 3.11 INSTALLATION CHECKOUT
- 3.11.1 Functional Checks
- 3.11.2 Ground Checks
- 3.11.3 Electromagnetic Interference (E.M.I.) Check
- 3.11.4 Panel mount NGT-9000 Display Check
- 3.11.5 Flight Test
- 3.11.6 Installation Checkout Complete
- 17001_4_Maint
- 17001_5_App-A_signal
- A.1 INTRODUCTION
- A.2 INPUT AND OUTPUT INTERFACES
- A.2.1 Input Power
- A.2.2 RF Suppression Bus
- A.2.3 Audio Output
- A.2.4 Gillham Input (Altitude Input)
- A.2.5 RS-232 Interface
- A.2.6 RS-422 Interface
- A.2.7 ARINC 429 Input
- A.2.8 ARINC 429 Output
- A.2.9 Discrete Input
- A.2.10 Discrete Output
- A.2.11 I2C Serial Bus (Detachable Configuration Module)
- A.2.12 Antenna Connections
- A.3 PIN DEFINITION SUMMARY
- A.4 [J1 CONNECTOR]
- 17001_6_App-B_Environmental
- 17001_7_App-C_Compatibility
- 17001_8_App-D_TSO
- 17001_9_App-E_Questionaire
Lynx NGT-9000
Installation Manual
0040-17001-01 (Revision W) Installation Page 2-32
2.3.11.4 Installation
1. Use the following information to the extent necessary to install the directional antenna.
• Standard installation practices prescribed in FAA Advisory Circular 43.13 must be followed.
• The installer must ensure the immediate antenna installation area is clean and prepared so that
the antenna is electrically bonded (metal-to-metal contact) to the aircraft. To provide optimum
bonding through the mounting holes, prepare the surfaces with Alodine No. 1001.
• To facilitate mounting to the airframe, the dimensions shown in Figure 2-19 can be used to
locate and drill mounting and connector access holes.
• Connection to the antenna should be made in accordance with the system interconnect diagram
Figure 2-6.
NOTE
A doubler plate (not supplied) is required to reinforce the aircraft skin.
2. Connect each of the three antenna cables. Check to ensure that each cable is connected to the correct
antenna connector. Each connector/cable has a matching color band (see note paragraph.).
3. Attach the antenna to the aircraft, with the special adapter plate and o-ring, using 10-32 hardware
provided. See Figure 2-20.
NOTES
1. Before installing the antenna on an aircraft remove the tape, which
holds the O-RING gasket in place during shipment. If the O-ring is
in a separate bag, remove and install it in the O-ring groove on the
bottom of the antenna.
2. For pressurized aircraft, use a sealant that meets the requirements of
SAE AMS-S-8802 such as Flamemaster CS3204 class B. For non-
pressurized aircraft, use a non-corrosive sealant that meets the
physical requirements of MIL-A-46146 such as General Electric
RTV162.